# N301AE: Saab-Scania SAAB 340B, registration cancelled 2008-08-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 14, 2008 - Exported to: Australia - Status when cancelled: Triennial form not returned - Airframe: [Saab-Scania SAAB 340B](https://openairdocs.org/model/saab-scania-saab-340b) (registry code 7860101) - Data sheets: [TCDS A52EU](https://openairdocs.org/tcds/A52EU) (OpenAirDocs) - Serial number: 340B-301 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: June 24, 1992 - Certificate issued: May 15, 1998 - Last registry action: May 15, 2007 - Mode S code: A3230E - Owner when cancelled: [American Eagle Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20EAGLE%20AIRLINES%20INC) - Location: [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth) - Owner type: Corporation - Owner's area on the map: 32.8240° N, 97.0491° W: Placed by OpenAirDocs at the center of ZIP code 76155, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N301AE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=301AE - Page: https://openairdocs.org/deregistered/N301AE-2008-08-14 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Saab-Scania SAAB 340B: https://openairdocs.org/model/saab-scania-saab-340b.md ## Service difficulty reports (35) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SIMA200816502](https://openairdocs.org/sdr/SIMA200816502), Jun 6, 2008: FLOOR SUPPORT. CORRODED. DURING A HMBV INSPECTION, A PREVIOUS REPAIR ON THE GALLEY FLOOR FRAME 258.0 WAS FOUND CORRODED WITH LEVEL TWO CORROSION. REMOVED THE DAMAGED FILLER TO REMOVED T - [SDR SIMA200742301](https://openairdocs.org/sdr/SIMA200742301), Nov 5, 2007: BLEED VALVE. MALFUNCTIONED. BEFORE TAKEOFF CHECKLIST NOTED RIGHT BLEED VALVE NOT CLOSED FOUND CB H16 POPPED. CONTACTED MOC. ADVISED TO RESET CB. CB H16 POPPED A SECOND TIME. CREW ELECTED T - [SDR SIMA200629002](https://openairdocs.org/sdr/SIMA200629002), Oct 16, 2006: WARNING LIGHT. FALSE INDICATION. LAVATORY SMOKE LIGHT ON CENTRAL WARNING PANEL. NO SMOKE NOTED IN LAVATORY, ISSUED MEL 26-2. (M) - [SDR SIMA200620502](https://openairdocs.org/sdr/SIMA200620502), Jul 22, 2006: WINDSHIELD. FAILED. CAPT FORWARD WINDSHIELD OUTER PLY SHATTERED. (M) - [SDR SIMA200530001](https://openairdocs.org/sdr/SIMA200530001), Oct 24, 2005: ODOR. DETECTED. FOUND CREW REPORTED STRONG SMOKE SMELL IN COCKPIT AND FORWARD CABIN. FOLLOWED CHECKLIST AND COULD NOT DETERMINE SOURCE. INSPECTED AVIONICS RACK AIR DISTRIBUTION - [SDR SIMA200520301](https://openairdocs.org/sdr/SIMA200520301), Jul 15, 2005: LINE. RUPTURED. DISC, UPON GEAR SELECTION UP THE HYDRAULIC QUANTITY STARTED DROPPING TO -0-, MANUAL PUMP OVERRIDE FAILURE. REPLACED RUPTURED NOSE LANDING GEAR RETRACT/EXTENSION - [SDR SIMA200518608](https://openairdocs.org/sdr/SIMA200518608), Jun 29, 2005: SKIN. CHAFED. THE LT IB NACELLE WAS FOUND CHAFED AT THE FILLET FAIRING SEAL CONTACT POINT. BLENDED THE DAMAGED AREA. FABRICATED AND INSTALLED A REPAIR DOUBLER. WORK DONE IAW - [SDR SIMA200518606](https://openairdocs.org/sdr/SIMA200518606), Jun 23, 2005: FLOORBEAM. CORRODED. FLOORBEAM AT STA 225.0 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. FABRICATED A FILLER, DOUBLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K) - [SDR SIMA200518605](https://openairdocs.org/sdr/SIMA200518605), Jun 23, 2005: FLOORBEAM. CORRODED. THE GALLEY FLOOR FRAME AT STA 272 WAS FOUND CORRODED. BLENDED THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (K) - [SDR SIMA200518604](https://openairdocs.org/sdr/SIMA200518604), Jun 23, 2005: FRAME. DAMAGED. THE CARGO SIDEWALL FRAME AT STA 686.888 WAS FOUND BENT AND DENTED. RECONTOURED THE FRAME. PREPARED AND INSTALLED REPAIR SECTION OF NEW FRAME. REPAIR DONE IAW SR - [SDR SIMA200518603](https://openairdocs.org/sdr/SIMA200518603), Jun 22, 2005: FRAME. DAMAGED. THE CARGO SIDEWALL FRAME AT STA 640 WAS FOUND DENTED. RECONTOURED THE DENT. FABRICATED AND INSTALLED REPAIR SECTION OF NEW FRAME. REPAIR DONE IAW SRM. (K) - [SDR SIMA200518602](https://openairdocs.org/sdr/SIMA200518602), Jun 22, 2005: FRAME. CORRODED. THE RT SIDEWALL CARGO FRAME AT STA 677 WAS FOUND DENTED. RECONTOURED THE DENT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (K) - [SDR SIMA200518601](https://openairdocs.org/sdr/SIMA200518601), Jun 22, 2005: WEB. CORRODED. THE REINFORCEMENT WEB AT STA 294 WAS FOUND CORRODED. BLENDED THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW REPAIR. (K) - [SDR SIMA200518607](https://openairdocs.org/sdr/SIMA200518607), Jun 21, 2005: FLOORBEAM. DAMAGED. THE CARGO FLOOR FRAME AT STA 710.0 WAS FOUND BENT IN 2 AREAS. RECONTOURED BOTH DENTS. FABRICATED AND INSTALLED 2 DOUBLERS AND 2 ANGLES. REPAIR DONE IAW SRM. (K) - [SDR SIMA200536101](https://openairdocs.org/sdr/SIMA200536101), Dec 22, 2004: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS AT ROW 9 AND 10 WILL NOT ILLUMINATE DURING TEST. EXIT SIGN OVER SEAT 8A DOES NOT ILLUMINATE. REPLACED BATTERY PACK. IAW MM OPERATIONAL CHECK GO - [SDR SIMA200111802](https://openairdocs.org/sdr/SIMA200111802), Apr 28, 2001: LIGHT. INOPERATIVE. LAX - FLT 3067 - EMERGENCY ARMED LIGHT INOPERATIVE ON FLIGHT ATTENDANTS PANEL. REMOVED AND REPLACED BULB IAW AMM 23-30-00. (M) - [SDR SIMA0622](https://openairdocs.org/sdr/SIMA0622), Mar 3, 2001: WARNING LIGHT. ILLUMINATED. DFW - FLT 3769 - ON APPROACH, WHEN GEAR WAS LOWERED CREW RECEIVED AN ANTI-SKID CAUTION INDICATION ON CWP. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK - [SDR SIMA0503](https://openairdocs.org/sdr/SIMA0503), Feb 19, 2001: POWER SUPPLY. DISCHARGED. JFK - FLT 5013 - CREW REPORTED THE EMERGENCY LIGHT OVER CABIN DOOR IS DIM AND FLICKERS. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT 21LN. OPERATIONAL CHE - [SDR SIMA2914](https://openairdocs.org/sdr/SIMA2914), Oct 17, 2000: LIGHT. MALFUNCTIONED. PVD - FLT 5045 - CREW REPORTED EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY, SUSPECT BATTERIES RECHARGED DURING FERRY FLIGHT. EME - [SDR SIMA2552](https://openairdocs.org/sdr/SIMA2552), Sep 11, 2000: BULB. INOPERATIVE. ALB - FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 7BC IS INOPERATIVE. MAINTENANCE REPLACED BULB IN FLOOR LIGHT AT SEAT 7BC. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT - [SDR SIMA1611](https://openairdocs.org/sdr/SIMA1611), Jun 9, 2000: CONTROL PANEL. INOPERATIVE. JFK - FLT 5069 - ABORTED TAKEOFF DUE TO CONFIGURATION WARNING, SPLIT PITCH, STANDBY UNCOMMANDED MOVEMENT. C/A - REPLACED TRIM CONTROL PANEL IAW SAAB340BA MM 27- - [SDR SIMA1383](https://openairdocs.org/sdr/SIMA1383), May 17, 2000: HANDLE. INOPERATIVE. JFK - FLT 5143 - RIGHT LANDING LIGHT DID NOT ILLUMINATE WHEN GEAR HANDLE WAS SELECTED DOWN. ABORTED APPROACH. AIRCRAFT WENT AROUND AND CREW PERFORMED LANDING GE - [SDR SIMA0821](https://openairdocs.org/sdr/SIMA0821), Mar 22, 2000: BULB. INOPERATIVE. DFW - FLT 3679 - EMERGENCY FLOOR LIGHT AT 9B INOPERATIVE. REMOVED AND REPLACED BULB AT 9B. OPS CHECK GOOD. (M) - [SDR SIMA3641](https://openairdocs.org/sdr/SIMA3641), Dec 28, 1999: CONNECTOR. DISCONNECTED. DFW - FLT 3296 - UNSAFE RIGHT GEAR INDICATION. PERFORMED EMERGENCY PROCEDURES. PULLED EMERGENCY HANDLE FOR GEAR DOORS. AIRCRAFT LANDED WITHOUT EVENT. INSPECTED - [SDR SIMA992652](https://openairdocs.org/sdr/SIMA992652), Sep 22, 1999: WIRE. BROKEN. JFK - FLT 5006 - EMERGENCY OVERHEAD LIGHTS AT SEATS 8BC, 10BC, AND 12 BC DO NOT ILLUMINATE. REPAIRED BROKEN WIRES AT FUSE HOLDERS 71 AND 72 LN. OPERATIONAL CHEC - [SDR SIMA992231](https://openairdocs.org/sdr/SIMA992231), Aug 11, 1999: BRAKES. REQ'D SERVICE. JFK - FLT 4925 - LEFT BRAKE GRABS EXCESSIVELY. RIGHT BRAKE DOES NOT GRAB AT ALL. INSPECTED AND BLED ALL FOUR BRAKES. LEAK AND FUNCTIONAL CHECK GOOD. AIRCRAFT RE - [SDR SIMA990893](https://openairdocs.org/sdr/SIMA990893), Mar 30, 1999: ANGLE. CHAFED. ABI - DURING A MBV INSPECTION, FOUND CHAFE ON THE LEFT NACELLE INLET COMPARTMENT LOWER LONGERON. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTIO - [SDR SIMA990892](https://openairdocs.org/sdr/SIMA990892), Mar 30, 1999: SKIN. CHAFED. ABI - DURING A MBV INSPECTION, FOUND CHAFE ON THE LEFT NACELLE OUTBOARD INNER SKIN. BLENDED THE CHAFE AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDI - [SDR SIMA990891](https://openairdocs.org/sdr/SIMA990891), Mar 30, 1999: SKIN. DENTED. ABI - DURING A MBV INSPECTION, FOUND DENTS ON RIGHT FUSELAGE SKIN PANEL STATION 327.5 BETWEEN SL 1620 AND 1622. CLEANED AREA, CUT OUT DAMAGE, AND PERFORMED AN E - [SDR SIMA983121](https://openairdocs.org/sdr/SIMA983121), Nov 8, 1998: ENGINE. MALFUNCTIONED. ALB - FLT 4812 - EN ROUTE TO JFK FROM YUL, THE LEFT ENGINE OIL PRESSURE STARTED DROPPING. WHEN IT GOT TO THE BOTTOM OF THE GREEN ARC, THEY SHUT DOWN THE ENGIEN - [SDR SIMA980862](https://openairdocs.org/sdr/SIMA980862), Mar 27, 1998: BULB. FAILED. DFW - FLT 3935 - WHITE FLOOR LIGHT NEAR ROW 10 INOP MEL'D PER 33-15-2. RETURNED A/C TO SERVICE. RAID BULB AT ROW 10 ON THE FLOOR PROX LIGHTING. PERFORMED OPERAT - [SDR SIMA980102](https://openairdocs.org/sdr/SIMA980102), Jan 10, 1998: CONNECTOR. LOOSE. DFW - FLT 3775 - LEFT OVERWING EMERGENCY LIGHT IS INOP. MAINTENANCE FOUND CONNECTOR PIN HAD BACKED OUT IN CONNECTOR AT LIGHT ASSY. REINSTALLED PIN IN CONNECTOR, - [SDR SIMA952661](https://openairdocs.org/sdr/SIMA952661), Sep 23, 1995: ENGINE. SEIZED. DFW - FLT NR 3503 - DURING TAKEOFF ENGINE NR 2 LOST POWER, TAKEOFF ABORTED. MAINTENANCE FOUND FIRST STAGE ROTOR DAMAGED. MAINTENANCE REPLACED NR 2 ENGINE. OPS C - [SDR SIMA952341](https://openairdocs.org/sdr/SIMA952341), Aug 22, 1995: SMOKE DETECTOR. MALFUNCTIONED. SGF - FLT NR 4186 - DURING TAKEOFF ROLL, THE AFT SMOKE DETECTOR LIGHT ILLUMINATED, THE TAKEOFF WAS ABORTED AND THE AFT CARGO FIRE BOTTLE WAS DISCHARGED. MAINTEN - [SDR SIMA950991](https://openairdocs.org/sdr/SIMA950991), Apr 9, 1995: HMU. MALFUNCTIONED. ORD - FLT 4351 - DURING CRUISE FLIGHT, PILOT UNABLE TO CONTROL ENGINE NR 2 TORQUE WITH POWER LEVER, TORQUE WAS FIXED AT 8046. TORQUE MOTOR LOCK-OUT NO EFFECT. F ## Other aircraft with N301AE - [Registered now](https://openairdocs.org/aircraft/N301AE): Mitsubishi MU-300, S/N A091 S.A. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.